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  9. Piper Aircraft Corporation ARCHER II PA-28-181 User manual

Piper Aircraft Corporation ARCHER II PA-28-181 User manual

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PIPER AIRCRAFT CORPORATION
PA-2&lu, ARCHER II SECTION T
GENERAL
SECTION 1
GENERAL
1.1 INTRODUCTION
This Pilot's Operating Handbook is designed for maximum utilization
as an op€rating guide for the pilot. It includes the material required to be
furnished to the pilot by C.A.R. 3 and FAR Part2l, Subpart J. It also
contains sripplemental data supplied by the airplane manufacturer.
This handbook is not designed as a substitutc for adequate and
competent flight instruction, knowledge of current airworthiness directives,
applicable federal air regulations or advisory circulars. It is not intended to
be a guide for basic flight instruction or a training manual and should not be
used for operational purposes unless kept in a current status.
Assurance that the airplane is in an airworthy condition is thc
responsibility of the owner. The pilot in command is responsible for
determining that the airplane is safe for flight. The pilot is also responsible
for remaining within the operating limitations as outlined by instrument
markings, placards, and this handbook.
Although the arrangement of this handbook is intended to increase its
in-flight capabilities, it should not be used solely as an occasional operating
reference. The pilot should study the entire handbook to familiarize himself
with the limitations, performance, procedures and operational handling
characteristics of the airplane before flight.
The handbook has been divided into numbered (arabic) sections, each
provided with a "finger-tip" tab divider lbr quick reference. The limitations
and emergency procedures have been placed ahead of the normal
procedures, performance and other sections to provide easier access to
information that may be required in flight. The "Emergency Procedures"
Section has been furnished with a red tab divider to present an instant
reference to the section. Provisions for expansion of the handbook have
been made by the deliberate omission of certain paragraph numbers, figure
numbers, item numbers and pages noted as being intentionally left blank.
REPORT: VF1120
1-l
ISSUED: JULY 2,1979
SECTION 1
GENERAL
PIPER AIRCRAFT CORPORATION
PA-2&1t1, ARCHER II
I\
t2'
te' !.0t"
THREE VIEW
Figure l-l
Wing Area (sq. ft.)
Min. Turning Radius (ft.)
(from pivot point to wingtip)
z',
170.0
30.0
I'
8.20"
I'
Lll"
REPORT: VB-1120
t-2 ISSUED: JULY 2,1979
PIPER AIRCRAFT CORPORATION
PA-28-181, ARCHER II SECTION 1
GENERAL
I.3 ENGINES
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model Number
(d) Takeoff Power - 5 Minute Limit (BHP)
(e) Takeoff Engine Speed - 5 Minute
Limir (RPM)
(f) Maximum Continuous Power (BHP)
(g) Maximum Continuous Engine
Speed (RPM)
(h) Bore (inches)
(i) Stroke (inches)
0) Displacement (cubic inches)
(k) Compression Ratio
(l) Engine Type
I.5 PROPELLERS
(a) Number of Propellers
(b) Propeller Manufacturer
(c) Model
(d) Number of Blades
(e) Propeller Diamete r (inches)
(l) Maximum
(2) Minimum
(f) Propeller Type
I.7 FUEL
AVCAS ONLY
(a) Fuel Capacity (U.S. gal.) (rorat)
(b) Usable Fuel (U.S. gal.) (total)
(c) Fuel
(l) Minimum Octane
(2) Alternate Fuel'
ISSUED: JULY 2,1979
REVfSED: JUNE 29,1984
2650
5.t25
4.375
36 r.0
8.5: I
Four Cylinder, Direct
Drive, Horizontally
Opposed, Air Cooled
I
Sensenich
76EM8S5-0-62
2
76
76
Fixed Pitch
100 Green or l00LL Blue
Aviation Grade
Refer to latest issue of
Lycoming lnstruction No. 1070.
REPORT: VB-I120
'1-3
I
Lycoming
0-360-44M or
o-360-A4A
t80
2700
t78
50
48
SECTION 1
GENERAL
PIPER AIRCRAFT CORPORATION
PA-28-181, ARCHER II
r.9 orl,
(a) Oil Capacity (U.S. quarts)
(b) Oil Specification
(c) Oil Viscosity per Average Ambient
Temp. for Starting
(l) Above 600F
(2) 30'F to 90oF
(3) 0oF to 70oF
(4) Below l0oF
1.11 MAXIMUM WEIGHTS
(a) Maximum Ramp Weight (lbs.)
(b) Maximum Takeoff Weight (lbs.)
(c) Maximum Landing Weight (lbs.)
(d) Maximum Weights in Baggage
Compartment (lbs.)
REPORT: VB-1120
l-4
200 0
ISSUED: JULY 2,1979
REVISED: JULY 21,1982
8
Refer to latest issue
of Lycoming Service
Instruction 1014.
Single
s.A.E. 50
s.A.E.40
s.A.E. 30
s.A.E. 20
Multi
S.A.E. 40 or 50
s.A.E.40
S.A.E.40 or
20w-30
s.A.E.20W-30
Normal
2558
2550
2550
Utility
2138
2130 ,
2130
1.13 STANDARD AIRPLANE WEIGHTS
Refer to Figure 6-5 for the Standard Empty Weight and the Useful
Load.
PIPER AIRCRAFT CORPORATION
PA-2t-1t1, ARCHER II SECTION 1
GENERAL
1.I5 BAGGAGE SPACE
(a) Compartment Volume (cubic feet)
(b) Entry Width (inches)
(c) Entry Height (inches)
r.17 SPECIFIC LOADINGS
(a) Wing Loading (lbs. per sq. ft.)
(b) Power Loading (lbs. per hp)
24
22
20
15.0
14.2
REPORT: VB-1120
1-5
ISSUED: JULY 2,1979
PIPER AIRCRAFT CORPORATION
PA-28-181, ARCHER II SECTION 2
LIMITATIONS
SECTION 2
LIMITATIONS
2.I GENERAL
This section provides the "FAA Approved" operating limitations, ,
instrument markings, color coding and basic placards necessary for opera- |
tion of the airplane and its systems.
This airplane must be operated as a normal or utility category airplane
in compliance with the operating limitations stated in the form of placards
and markings and those given in this section and this complete handbook.
Limitations associated with those optional systems and equipment
which require handbook supplements can be found in Section 9
(Supplements).
2.3 AIRSPEED LIMIT'ATIONS
SPEED KIAS KCAS
Neve5 Exceed Speed (VNE) - Do not exceed
this speed in any operation.
Maximum Structural Cruising Speed
(VNO) - Do not exceed this speed except in
smooth air and then only with caution.
t54 148
t25 t2t
REPORT: VB-1120
2-l
ISSUDD: JULY 2,1979
REVISED: JULY 21, 1982
SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-2&1t1, ARCHER II
SPEED
Design Maneuvering Speed (VA) - Do not
make full or abrupt control movements
above this speed.
At 2550lbs. G.W.
At 1634lbs. G.W,
KIAS KCAS
lr3
89
lil
89
CAUTION
Maneuvering speed decreases at lighter weight
as the effects of aerodynamic forces become
more pronounced. Linear interpolation may be
used for intermediate gross weights. Maneuver-
ing speed should not be exceeded while opera-
ting in rough air.
Maximum Flaps Extended Speed
Do not exceed this speed with the
extended. t02 100
IAS
154 KTS
125 KTS to
I54 KTS
55 KTS to
I25 KTS
49 KTS to
IO2 KTS
(vFE)
flaps
2.5 AIRSPEED INDICATOR MARKINGS
MARKING
Red Radial Line (Never Exceed)
Yellow Arc (Caution Range - Smooth
Air Only)
Green Arc (Normal Operating Range)
White Arc (Flap Down)
REPORT: VBll2O
2-2
ISSUED JULY 2, t979
PI PER AIRCRAFT CORPORATION
PA.28-I8I, ARCHER II
SECTION 2
I-IMITATIONS
2.7 POWER PLANT LIMITATIONS
(a) Nurrrbcrol'Engincs
(b) Engine Manufacturcr
(c) Engine Modcl No.
(d) Engine Operating Limits
( l) Takcofl'Power - 5 Minute
limit (BHP)
(2) Takeoff Engine Speed - 5
Minute Limit (RPM)
(3) Maximum Continuous Power
(BHP)
(4) Maximum Continuous Engine
Speed (RPM)
(5) Maximum Oil Temperature
(6) Oil Pressure
Minimum (red line)
Maxinrum (red line)
(7) Fuel Pressure
Minimum (red line)
Maximum (red line)
(8) Fuel(AVGAS ONLY)
(minimum grade)
(9) Number of Propellers
( l0) Propeller Manufacturer
(l l) Propeller Model
( l2) Propeller Diameter
Minimum
Maximum
( l3) Propeller Tolerancc (static RPM
at maximum pennissible throttle
setting, sea level, ISA)
ISSUED: JULY 2,1979
REVTSED; APRIL 2,1998
NOTE
Rel'er to the airplane maintenance manual for tcst
procedurc to determine approved static rpm
under non-standard conditions.
I
Lycoming
O-360-A4M or
O-360-A4A with
carburctor setting
r0-3878
180
27m
178
2650
245"F
25 PSI
90 or l0O PSI
0.5 PSI
8 PSI
100 or l00LL
Aviation Grade
I
Sensenich
76EM8S5-0-62
76IN
76IN
Not above 2340 RPM
Not below 2240 RPM
REPORT: VB-1r20
2-3
SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-28.I8I, ARCHER II
2.9 POWBR PLANT INSTRUMENT MARKINGS
(a) Tachonreter
Green Arc (Normal Operating Rango)
Yellow Arc (5 Minute Limit)
Red Line (Takeoff Power)
(b) OilTemperature
Grcen Arc (Normal Operating Range)
Red Line (Maximum)
(c) Oil Pressure
Green Arc (Normal Operating Range)
Yellow Arc (Caution Range) (Idle)
Yellow Arc (Ground Warm-Up)
Red Line (Minimum)
Red Line (Maximum)
(d) Fuel Pressure
Green Arc (Normal Operating Range)
Red [,ine (Minimum)
Red Line (Maximum)
500 r() 2650 RPM
2650 to 2700 RPM
27OO RPM
75' to 245"F
245"F
60 PSI tO 90 PSI
25 PSI to 60 PSI
None or 90 PSI to 100 PSI
25 PSI
90 or 100 PSI
0.-5 PSI to 8 PSI
0.5 PSI
8 PSI
Utility
2.I1 WEIGHT LIMITS
Normal
(a) Maxirnum Ramp (lbs.) 2558
(b) Maximum Weight (lbs.) 2550
(c) Maximum Baggage (lbs.) 2ü)
NOTE
Refer to Section 5 (Performance) frrr maximum
rveight as limited by performanco.
REPORT: VB-1r20
2138
2 t30
0
ISSUED: JULY 2,1979
a^ Dr|ltroDn- rrrr t/ al iator
PIPER AIRCRAFT CORPORATION
PA-2&1ü, ARCHER II SECTION 2
LIMITATIONS
2.13 CENTER OF GRAVITY LIMITS
(a) Normal Category
Weight
Pounds
Forward Limit
Inches Aft of Datum
Rearward Limit
Inches Aft of Datum
2550
2050 (and
less)
88.6
82.0
93.0
93.0
(b) Utility Category
Weight
Pounds
Forward Limit
Inches Aft of Datum
Rearward Limit
Inches Aft of Datum
2t30
2050 (and
less)
83.0
82.0
93.0
93.0
NOTES
Straight line variation between points given.
The datum used is 78.4 inches ahead of the wing
leading edge at the inboard intersection of the
straight and tapered section.
It is the responsibility of the airplane owner and
the pilot to insure that the airplane is properly
loaded. See Section 6 (Weight and Ralance) for
proper loading instructions.
REPORT: VFll2O
2-S
ISSUED: JULY 2,1979